View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 28353U 26159.11015513 +.00000000 +00000-0 -86694-4 0 00002
2 28353 71.0021 42.7392 0007495 265.8006 94.2259 14.14612296 00
| Epoch (UTC): | 08 June 2026 02:38:37 |
| Eccentricity: | 0.0007495 |
| inclination: | 71.0021° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 42.7392° |
| argument of perigee: | 265.8006° |
| revolutions per day: | 14.14612296 |
| mean anomaly at epoch: | 94.2259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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